step 1:
Step 2: As K and 1/s(s+2) are in cascade so their equivalent is = K/s(s+2),
Step 3: Eliminate the summing point, therefore tranfer function is:-
C(s)/R(s) = (K/s(s+2)) / (1+(K/s(s+2))*(1+ks))
on simplifying we get,
C(s)/R(s) = K / (s^2 +2s +K + Kks) = K / (s^2 + (2+Kk)s + K)
Now the characteristic equation is:
s^2+(2+Kk)s+K=0
?n = K^(0.5)
5 = K^(0.5)
K= 25
and
£ = 0.7 (given)
Now,
2£?n = 2+Kk
2*0.7*5 = 2+25*k
k= 0.2
Now,
Settling time,
tn = 4/£?n
= 4/0.7*5
= 1.143
System Dynamics
3. Determine the values of K and k such that the closed-loop system shown in the Figure has a damping ratio ? of 0.7 and an undamped natural frequency en of4 rad/s R(s) 1 C(s)
Problem 3: (30 Consider a block diagram which represents the satellite control system with a controller Ge(s) (a) Assuming no initial conditions, find the output response y(t) when the impulse input is applied to the system, where Gc(s) is a proportional gain K. (10) (b) Design a lead-compensator Ge(s) for which the complex pole of the closed-loop system has 0.5 of damping ratio () and 2 rad/s of undamped natural frequency (on) (The zero of a lead-compensator is given as...
Question three The figure below shows a unit step response of a second order system. From the graph of response find: 1- The rise timet, 2- The peak timet, 3- The maximum overshoot Mp 4- The damped natural frequency w 5. The transfer function. Hence find the damping ratio ζ and the natural frequency ah-Find also the transfer function of the system. r 4 02 15 25 35 45 Question Four For the control system shown in the figure below,...
K and consider a PI s+4 A unity feedback system has an open loop transfer function G(s) [4] S+a controller Ge(s) S Select the values of K and a to achieve a) (i) Peak overshoot of about 20% (ii) Settling time (2% bases) ~ 1 sec b) For the values of K and a found in part (a), calculate the unit ramp input steady state error
K and consider a PI s+4 A unity feedback system has an open loop...
Q3. Consider a single loop unity feedback control system of the open loop transfer function (a) Find the range of values of the gain K and the parameter p so that: (i) The overshoot is less than 10%. (ii)The settling time is less than 4 seconds Note: , 4.6 M. = exp CO 40% (b)What are the three elements in a PID controller? Considering each in turn, explain the main ways in which varying the parameters affects the closed-loop system...
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1. Given the following unity feedback system where s+z s2 (s + 10) and the controller is a proportional controller Ge = K, do the following: a. If z = 2, find K so that the damped frequency of the oscillation of the transient response is 5 rad/s. b. The system is to be redesigned by changing the values of z and K. If the new...
Determine: 1. The transfer function C(s)/R(s). Also find the
closed-loop poles of the system. 2. The values of the undamped
natural frequency ωN and damping ratio ξ of the closed-loop poles.
3. The expressions of the rise time, the peak time, the maximum
overshoot, and the 2% settling time due to a unit-step reference
signal.
For the open-loop process with negative feedback R(S) Gp(S) C(s) H(s) 103 Go(s) = 1 , Gp(s)- s(s + 4) Determine: 1. The transfer function...
Referring to the system shown in Figure (a), determine the values of K and k such that the system has a damping ratio 5 of 0.7 and an undamped natural frequency wn of 4 radsec. R(S) C(s) K S + 2 k Select one: O a. K=0.249 and k=0.178 O b. K = 16 and k=0.225 Oc. K=0.467 and k=0.874 O d. K = 0.367 and k=12 O e. K=12 and k=18
Problem Consider the system shown in Figure 5–74(a). The damping ratio of this system is 0.158 and the undamped natural frequency is 3.16 rad/sec. To improve the relative stability, we employ tachometer feedback. Figure 5–74(b) shows such a tachometer-feedback system. Determine the value of Kn so that the damping ratio of the system is 0.5. Draw unit-step response curves of both the original and tachometer-feedback systems. Also draw the error-versus-time curves for the unit-ramp response of both systems. R(3) C(s)...
Design a controller for the transfer function)5)(1(1)(++=sssGto obtain (i) zero steady-stateerror due to step, (ii) a settling time of less than 2 s, and (iii) an undamped natural frequency of 5 rad/s. Obtain the response due to a unit step and find the percentage overshoot, the time to the first peak and steady-state error percent due to a ramp input